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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 500,000
Max Cl/Cd: 109.59 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx83w160-il-500000.txt
Download as CSV file: xf-fx83w160-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 83-W-160                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.7562   0.11278   0.10954  -0.0743   1.0000   0.0246
 -18.250  -0.7868   0.10382   0.10042  -0.0788   1.0000   0.0247
 -18.000  -0.8044   0.09768   0.09419  -0.0817   1.0000   0.0248
 -17.750  -0.8195   0.09213   0.08855  -0.0842   1.0000   0.0250
 -17.500  -0.8348   0.08677   0.08311  -0.0864   1.0000   0.0252
 -17.250  -0.8468   0.08213   0.07840  -0.0883   1.0000   0.0254
 -17.000  -0.8587   0.07770   0.07389  -0.0899   1.0000   0.0257
 -16.750  -0.8717   0.07337   0.06947  -0.0912   1.0000   0.0259
 -16.500  -0.8846   0.06931   0.06533  -0.0922   1.0000   0.0262
 -16.250  -0.8967   0.06566   0.06159  -0.0929   1.0000   0.0265
 -16.000  -0.9103   0.06220   0.05805  -0.0929   1.0000   0.0266
 -15.750  -0.9231   0.05918   0.05494  -0.0927   1.0000   0.0268
 -15.500  -0.9293   0.05578   0.05142  -0.0943   0.9995   0.0273
 -15.250  -0.9224   0.05219   0.04769  -0.0982   0.9978   0.0276
 -15.000  -0.9149   0.04868   0.04402  -0.1024   0.9958   0.0280
 -14.750  -0.9049   0.04586   0.04117  -0.1053   0.9939   0.0287
 -14.500  -0.8925   0.04335   0.03861  -0.1081   0.9912   0.0293
 -14.250  -0.8777   0.04097   0.03617  -0.1113   0.9888   0.0298
 -14.000  -0.8606   0.03872   0.03384  -0.1146   0.9869   0.0304
 -13.750  -0.8450   0.03656   0.03158  -0.1174   0.9840   0.0311
 -13.500  -0.8281   0.03458   0.02947  -0.1201   0.9802   0.0319
 -13.250  -0.8071   0.03262   0.02739  -0.1233   0.9778   0.0326
 -13.000  -0.7868   0.03057   0.02533  -0.1264   0.9762   0.0336
 -12.750  -0.7732   0.02904   0.02377  -0.1274   0.9702   0.0343
 -12.500  -0.7500   0.02750   0.02217  -0.1301   0.9675   0.0352
 -12.250  -0.7229   0.02610   0.02067  -0.1333   0.9658   0.0365
 -12.000  -0.7035   0.02490   0.01936  -0.1346   0.9609   0.0374
 -11.750  -0.6868   0.02310   0.01754  -0.1363   0.9564   0.0387
 -11.500  -0.6604   0.02180   0.01621  -0.1392   0.9540   0.0401
 -11.250  -0.6292   0.02070   0.01503  -0.1423   0.9525   0.0418
 -11.000  -0.6142   0.02000   0.01423  -0.1414   0.9454   0.0431
 -10.750  -0.5884   0.01880   0.01303  -0.1433   0.9421   0.0453
 -10.500  -0.5561   0.01805   0.01224  -0.1456   0.9400   0.0476
 -10.250  -0.5229   0.01729   0.01140  -0.1479   0.9380   0.0502
 -10.000  -0.5110   0.01670   0.01081  -0.1459   0.9300   0.0527
  -9.750  -0.4810   0.01618   0.01024  -0.1472   0.9266   0.0557
  -9.500  -0.4509   0.01552   0.00955  -0.1487   0.9237   0.0593
  -9.250  -0.4297   0.01516   0.00918  -0.1480   0.9184   0.0626
  -9.000  -0.4060   0.01478   0.00873  -0.1477   0.9133   0.0661
  -8.750  -0.3784   0.01423   0.00819  -0.1484   0.9095   0.0707
  -8.500  -0.3461   0.01384   0.00773  -0.1499   0.9065   0.0754
  -8.250  -0.3311   0.01347   0.00740  -0.1478   0.9000   0.0801
  -8.000  -0.3041   0.01321   0.00708  -0.1480   0.8957   0.0852
  -7.750  -0.2762   0.01276   0.00665  -0.1486   0.8921   0.0925
  -7.500  -0.2500   0.01250   0.00636  -0.1486   0.8879   0.0989
  -7.250  -0.2286   0.01223   0.00611  -0.1477   0.8827   0.1059
  -7.000  -0.2022   0.01194   0.00580  -0.1477   0.8786   0.1137
  -6.750  -0.1731   0.01169   0.00554  -0.1483   0.8753   0.1227
  -6.500  -0.1469   0.01140   0.00528  -0.1483   0.8715   0.1334
  -6.250  -0.1247   0.01117   0.00507  -0.1474   0.8667   0.1435
  -6.000  -0.0983   0.01093   0.00483  -0.1473   0.8625   0.1558
  -5.750  -0.0702   0.01065   0.00457  -0.1477   0.8590   0.1707
  -5.500  -0.0415   0.01037   0.00434  -0.1482   0.8556   0.1905
  -5.250  -0.0200   0.01011   0.00418  -0.1472   0.8512   0.2145
  -5.000   0.0051   0.00981   0.00398  -0.1469   0.8471   0.2443
  -4.750   0.0320   0.00950   0.00378  -0.1471   0.8436   0.2836
  -4.500   0.0607   0.00921   0.00362  -0.1476   0.8404   0.3277
  -4.250   0.0856   0.00901   0.00353  -0.1472   0.8365   0.3643
  -4.000   0.1102   0.00886   0.00347  -0.1466   0.8321   0.3972
  -3.750   0.1376   0.00874   0.00341  -0.1466   0.8281   0.4252
  -3.500   0.1671   0.00868   0.00336  -0.1469   0.8248   0.4478
  -3.250   0.1977   0.00869   0.00335  -0.1475   0.8216   0.4660
  -3.000   0.2218   0.00868   0.00338  -0.1467   0.8177   0.4802
  -2.750   0.2486   0.00870   0.00342  -0.1465   0.8139   0.4933
  -2.500   0.2773   0.00874   0.00345  -0.1466   0.8106   0.5069
  -2.250   0.3072   0.00880   0.00345  -0.1470   0.8076   0.5182
  -2.000   0.3384   0.00887   0.00350  -0.1477   0.8047   0.5267
  -1.750   0.3628   0.00893   0.00355  -0.1469   0.8011   0.5349
  -1.500   0.3891   0.00894   0.00359  -0.1465   0.7973   0.5413
  -1.250   0.4176   0.00898   0.00361  -0.1466   0.7938   0.5490
  -1.000   0.4471   0.00901   0.00363  -0.1469   0.7907   0.5566
  -0.750   0.4784   0.00911   0.00371  -0.1476   0.7876   0.5645
  -0.500   0.5020   0.00917   0.00377  -0.1466   0.7837   0.5715
  -0.250   0.5281   0.00917   0.00383  -0.1462   0.7798   0.5775
   0.000   0.5564   0.00920   0.00386  -0.1463   0.7762   0.5834
   0.250   0.5863   0.00927   0.00387  -0.1467   0.7731   0.5889
   0.500   0.6159   0.00928   0.00390  -0.1470   0.7697   0.5932
   0.750   0.6392   0.00929   0.00397  -0.1460   0.7652   0.5975
   1.000   0.6658   0.00930   0.00398  -0.1457   0.7603   0.6029
   1.250   0.6951   0.00931   0.00395  -0.1459   0.7558   0.6077
   1.500   0.7224   0.00932   0.00398  -0.1457   0.7513   0.6118
   1.750   0.7453   0.00928   0.00399  -0.1446   0.7446   0.6156
   2.000   0.7743   0.00924   0.00389  -0.1446   0.7368   0.6198
   2.250   0.7936   0.00921   0.00387  -0.1427   0.7274   0.6240
   2.500   0.8211   0.00918   0.00380  -0.1424   0.7195   0.6283
   2.750   0.8421   0.00917   0.00388  -0.1409   0.7127   0.6324
   3.000   0.8667   0.00919   0.00392  -0.1402   0.7069   0.6372
   3.250   0.8944   0.00925   0.00395  -0.1401   0.7013   0.6419
   3.500   0.9147   0.00925   0.00402  -0.1385   0.6937   0.6459
   3.750   0.9398   0.00927   0.00403  -0.1378   0.6860   0.6497
   4.000   0.9591   0.00929   0.00410  -0.1359   0.6766   0.6538
   4.250   0.9827   0.00935   0.00414  -0.1349   0.6677   0.6582
   4.500   1.0011   0.00939   0.00422  -0.1329   0.6571   0.6627
   4.750   1.0203   0.00944   0.00430  -0.1310   0.6462   0.6672
   5.000   1.0366   0.00951   0.00437  -0.1285   0.6338   0.6721
   5.250   1.0510   0.00959   0.00446  -0.1257   0.6199   0.6774
   5.500   1.0649   0.00972   0.00459  -0.1227   0.6037   0.6829
   5.750   1.0758   0.00994   0.00478  -0.1192   0.5829   0.6890
   6.000   1.0834   0.01025   0.00502  -0.1151   0.5543   0.6954
   6.250   1.0849   0.01074   0.00536  -0.1099   0.5170   0.7018
   6.500   1.0828   0.01140   0.00584  -0.1042   0.4736   0.7092
   6.750   1.0788   0.01224   0.00646  -0.0985   0.4269   0.7175
   7.000   1.0785   0.01305   0.00712  -0.0936   0.3871   0.7273
   7.250   1.0783   0.01395   0.00786  -0.0890   0.3471   0.7391
   7.500   1.0816   0.01478   0.00858  -0.0850   0.3120   0.7543
   7.750   1.0859   0.01559   0.00932  -0.0813   0.2809   0.7756
   8.000   1.0910   0.01632   0.01006  -0.0778   0.2546   0.8113
   8.250   1.1169   0.01707   0.01093  -0.0790   0.2223   0.9731
   8.500   1.1245   0.01786   0.01162  -0.0760   0.2046   1.0000
   8.750   1.1365   0.01869   0.01236  -0.0740   0.1878   1.0000
   9.000   1.1484   0.01953   0.01312  -0.0721   0.1737   1.0000
   9.250   1.1606   0.02038   0.01389  -0.0702   0.1613   1.0000
   9.500   1.1745   0.02115   0.01463  -0.0686   0.1506   1.0000
   9.750   1.1879   0.02197   0.01541  -0.0670   0.1413   1.0000
  10.000   1.2006   0.02284   0.01624  -0.0653   0.1327   1.0000
  10.250   1.2149   0.02364   0.01703  -0.0639   0.1255   1.0000
  10.500   1.2272   0.02457   0.01793  -0.0623   0.1182   1.0000
  10.750   1.2415   0.02541   0.01878  -0.0610   0.1123   1.0000
  11.000   1.2542   0.02635   0.01970  -0.0595   0.1061   1.0000
  11.250   1.2670   0.02731   0.02066  -0.0581   0.1006   1.0000
  11.500   1.2803   0.02825   0.02160  -0.0568   0.0952   1.0000
  11.750   1.2912   0.02937   0.02271  -0.0553   0.0900   1.0000
  12.000   1.3052   0.03031   0.02367  -0.0542   0.0853   1.0000
  12.250   1.3146   0.03158   0.02491  -0.0526   0.0806   1.0000
  12.500   1.3278   0.03261   0.02599  -0.0515   0.0769   1.0000
  12.750   1.3387   0.03381   0.02719  -0.0502   0.0728   1.0000
  13.000   1.3472   0.03524   0.02862  -0.0488   0.0693   1.0000
  13.250   1.3601   0.03634   0.02978  -0.0478   0.0663   1.0000
  13.500   1.3698   0.03771   0.03115  -0.0466   0.0630   1.0000
  13.750   1.3769   0.03933   0.03279  -0.0453   0.0602   1.0000
  14.000   1.3893   0.04053   0.03406  -0.0444   0.0575   1.0000
  14.250   1.3982   0.04204   0.03558  -0.0434   0.0549   1.0000
  14.500   1.4034   0.04392   0.03748  -0.0422   0.0526   1.0000
  14.750   1.4145   0.04530   0.03893  -0.0414   0.0503   1.0000
  15.000   1.4226   0.04698   0.04062  -0.0405   0.0479   1.0000
  15.500   1.4335   0.05092   0.04467  -0.0387   0.0444   1.0000
  15.750   1.4411   0.05275   0.04657  -0.0380   0.0428   1.0000
  16.000   1.4457   0.05491   0.04876  -0.0373   0.0414   1.0000
  16.250   1.4449   0.05768   0.05156  -0.0366   0.0399   1.0000
  16.500   1.4503   0.05986   0.05383  -0.0361   0.0388   1.0000
  16.750   1.4560   0.06202   0.05609  -0.0357   0.0377   1.0000
  17.000   1.4600   0.06444   0.05858  -0.0354   0.0366   1.0000
  17.250   1.4624   0.06709   0.06128  -0.0351   0.0356   1.0000
  17.500   1.4602   0.07032   0.06454  -0.0350   0.0345   1.0000
  17.750   1.4603   0.07333   0.06765  -0.0350   0.0337   1.0000
  18.000   1.4639   0.07600   0.07044  -0.0351   0.0328   1.0000
  18.250   1.4656   0.07895   0.07348  -0.0354   0.0320   1.0000
  18.500   1.4661   0.08210   0.07671  -0.0358   0.0312   1.0000
  18.750   1.4656   0.08546   0.08014  -0.0363   0.0306   1.0000
  19.000   1.4613   0.08938   0.08412  -0.0371   0.0299   1.0000
  19.250   1.4544   0.09364   0.08844  -0.0380   0.0293   1.0000
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